AeroTech Congress & Exhibition - SAE International Cutting and Trimming of the Carbon Fibre Wing...

Tuesday, September 18


Automated Machine Technologies (Part A)

Automated Machine Technologies (Part B)

Session Code:

Session Code:

ATC28

ATC29

Room 501A - B

Room 501A - B

This session presents new technologies and system configurations that have been introduced in "state of the art" automated machines to address thechanging assembly requirements and materials in today's airframes.

This session continues the presentation of new technologies and systems configuration in automated machines to demonstrate the latestadvancements in fastener machine designs and installations world wide.

Gordon L. Allen, Steven L. Brisben, Boeing Co.; Ken Benczkowski, Broetje Automation

Mark W. Smith, Lockheed Martin Aeronautics Co.; Steven L. Brisben, Gordon L. Allen, Boeing Co.;Archie D. Crowe, Lockheed Martin Corp. (retired)

Organizers -

Organizers -

1:30 p.m.

2:00 p.m.

2:30 p.m.

3:30 p.m.

4:00 p.m.

4:00 p.m.

4:30 p.m.

2007-01-3780

2007-01-3781

2007-01-3782

2007-01-3795

2007-01-3783

2007-01-3796

2007-01-3895

2007-01-3797

All Electric Fastening System (AEFS)

Development of Portable and Flexible Track Positioning System forAircraft Manufacturing Processes

Universal Splice Machine

Lug Cutting and Trimming of the Carbon Fibre Wing Panels of theAirbus A400m with Portable Hand Positioned Tools

Horizontal Rivet Injector Design Used on A320 Upper Panel

Automated Fastening for Complex Aircraft Structures

An Innovative Blind System to Hold Drilling JIGs

Flexible Fixtures with Low Cost and Short Lead-Times (Written Only --No Oral Presentation)

The papers in this session are available in a single publication, SP-2142, and also individually.

Planned by AeroFast International Committee / EMB Air and Space Group

Brian O'Rourke, Broetje Automation; Thorsten Dillhoefer, Broetje-Automation Gmbh

Eric M. Reid, Boeing Commercial Airplanes

Joerg Heithus, Broetje Automation; Patrick L. Wishall, Boeing Co.

Barry Richards, Electroimpact Inc.; Kenny Howard, Electroimpact UK;Stephen Williams, Airbus UK

Chris Bucheit, Peter B. Zieve, Electroimpact Inc.

Hans-Juergen Borchers, BROETJE-Automation GmbH

Alexis Gabillon, Blanc Aero

Henrik Kihlman, Linkoping Univ.; Magnus Engstrom, Saab AB

CANCELLED

ORAL ONLY

Time

Time

Paper No.

Paper No.

Title

Title

AeroTech Congress & ExhibitionTechnical Session Schedule

As of 09/23/2007 07:40 pm

1:30 p.m.

3:30 p.m.

Session Time:

Session Time:



Safety / Security: Airborne Network Security

Safety / Security: Safety of Distributed Integrated Systems

Session Code:

Session Code:

ATC110A

ATC110B

Room 503

Room 503

The development of a world-wide information network (i.e., the Internet) has led to increasing pressure to add Internet-compatible systems andnetworks to commercial air transports both for airline business reasons and for passenger use. Live off-board connectivity is a primary objective ofsuch efforts.

Increasingly popular over the last years in the automotive industry, distributed integrated architectures are becoming commonplace as IntegratedModular Avionics (or IMA) systems in today¿s (and tomorrow¿s) aircraft. In order to support safety critical functions, a distributed integratedarchitecture needs to embody fault-tolerance strategies that enable the continued operation of the system in the presence of failures. This sessionexplores the concept of fault containment regions in a distributed integrated architecture.

John C. Dalton, Boeing Co.; Dan Johnson, Honeywell; Andy Wallington, GE Aviation (formerlySmiths Aerospace)

John C. Dalton, Boeing Co.; Mirko Jakovljevic, TTTech. Computertechnik AG; Andy Wallington, GEAviation (formerly Smiths Aerospace)

Organizers -

Organizers -

1:30 p.m.

2:00 p.m.

2:30 p.m.

3:30 p.m.

4:00 p.m.

4:30 p.m.

2007-01-3784

2007-01-3785

2007-01-3786

2007-01-3798

2007-01-3799

2007-01-3800

Assessing the Security of Airborne Networks

Keep the User in Mind: Operational Considerations for SecuringAirborne Networks

PASA (Preliminary Airplane Safety Assessment), an Aircraft-LevelSafety Methodology

The Fault Assumptions in Distributed Integrated Architectures

Methodology for the Common Mode Analysis

A Tool-based Approach for Reliable Autonomy in Avionics



Planned by Safety Committee / EMB Air and Space Group


Daniel P. Johnson, Honeywell

Chuck Royalty, Boeing

Roger K. Nicholson, Boeing

Roman Obermaisser, P. Peti, Vienna University of Technology

Zdzislaw H. Klim, Bombardier Aerospace; Marek Balazinski, EcolePolytechnique de Montreal

Clemens Renner, University of Potsdam

ORAL ONLY

CANCELLED

Time

Time

Paper No.

Paper No.

Title

Title

1:30 p.m.

3:30 p.m.

Session Time:

Session Time:




System Architectures, Platform and Integration 1

System Architectures, Platform and Integration 2

General Aerodynamics

Session Code:

Session Code:

Session Code:

ATC2A

ATC2B

ATC12

Room 504

Room 504

Room 505

The advancement of modern technology has resulted in an increase in demand for more sophisticated and robust avionics systems. This hasincreased the need for distributed embedded computing systems where smart devices work together to perform complex operations to achieveadvanced mission objectives. This session provides insight into critical design principles for distributed avionics systems including contemporaryavionics bus/network technologies and distributed processing architectures.

The advancement of modern technology has resulted in an increase in demand for more sophisticated and robust avionics systems. This hasincreased the need for distributed embedded computing systems where smart devices work together to perform complex operations to achieveadvanced mission objectives. This session provides insight into critical design principles for distributed avionics systems including contemporaryavionics bus/network technologies and distributed processing architectures.

Mark Lawrence Darnell, GE Aviation; Mirko Jakovljevic, TTTech. Computertechnik AG

Roscoe C. Ferguson, United Space Alliance; Mirko Jakovljevic, TTTech. Computertechnik AG

Organizers -

Organizers -

1:30 p.m.

2:00 p.m.

3:30 p.m.

4:00 p.m.

4:30 p.m.

5:00 p.m.

ORAL ONLY

ORAL ONLY

2007-01-3801

2007-01-3802

ORAL ONLY

ORAL ONLY

Modern "Safety Critical" Control Systems for Commercial Aircrafts

Advanced Digital Position & Speed Measurement Sensor Technology

Buses and Networks for Contemporary Avionics

Subsystem Design and Integration of a Robust Modular Avionics Suitefor UAV Systems Using the Time Triggered Protocol (TTP)

Space Shuttle Avionics and Identical Inputs

Building and Testing Deterministic Fiber Optic Networks For Avionics

Planned by Avionics Committee / EMB Air and Space Group


Jean-Pierre Garcia, Messier-Bugatti

Derek S. Weber, Inprox Sensors; Brandt Taylor, Taylor Engineering

Mike S. Glass, Data Device Corp.

Allwyn Samuel, Nelson Brown, Richard D. Colgren, University of Kansas;Gene Kelly, CertTech LLC

Scott Cox, United Space Alliance

Ken Applebaum, Champion Optical Technology Services

Time

Time

Paper No.

Paper No.

Title

Title

1:30 p.m.

3:30 p.m.

1:30 p.m.

Session Time:

Session Time:

Session Time:



Flying Cars

Airbreathing Engine Systems

Session Code:

Session Code:

ATC20A

ATC35

Room 505

Room 506

The General Aerodynamics session is planned for aerodynamic related topics that do not fall into one of the specialized aerodynamic sessions.

This session will address the development of Personal Transportation vehicles and components, focusing on innovative CTOL and VTOL roadableairplanes and flying automobiles. Required technologies, alternative system configurations, designs under development, prototype hardware, and in-flight performance of remote controlled models and full size prototypes will be presented.

Reuben M. Chandrasekharan, Bombardier Learjet; George Howell, Lockheed Martin Aeronuatics

Reuben M. Chandrasekharan, Bombardier Learjet; Bruce Harman, Branko Sarh, Boeing Co.

Organizers -

Organizers -

1:30 p.m.

2:00 p.m.

2:30 p.m.

3:30 p.m.

4:00 p.m.

4:30 p.m.

5:00 p.m.

2007-01-3787

2007-01-3788

ORAL ONLY

2007-01-3803

ORAL ONLY

ORAL ONLY

ORAL ONLY

2007-01-3804

The Effects of Humidity on the Properties of Air and the Influence ofCondensation on the Pressure Distribution over an Aerofoil

A Brief Survey of the Experimental Methods used for Wake VortexInvestigations

Non-linear Unsteady Aerodynamic and Aeroelastic Computation ofAircraft Wings

Technologies for Capability-based Personal Air Vehicles

Development of Aerodynamic and Structural Inflatable Components forPersonal Air Transportation

The Transition: A Driving and Flying Vehicle Created by Terrafugia

A Hybrid Powerplant for Powered Lift Aircraft

Prediction of Susceptibility of Small Aircraft to Pilot-InducedOscillations (Written Only -- No Oral Presentation)

Planned by Flight Sciences Committee / EMB Air and Space Group


Dave Philpott, IHS ESDU

Kamran Rokhsaz, Linda Kliment, Wichita State Univ.

Piergiovanni Marzocca, Clarkson Univ.

Mark D. Moore, NASA Langley Research Center

Jamey D. Jacob, Oklahoma State Univ.

Sam Schweighart, Terrafugia

Paul S. Moller, Moller Intl.

Pawel Rzucidlo, Andrzej Tomczyk, Rzeszow University of Technology

ORAL ONLY

Time

Time

Paper No.

Paper No.

Title

Title

3:30 p.m.

1:30 p.m.

Session Time:

Session Time:



Unmanned/Autonomous and Automatic Vehicle Control

Product Lifecycle Management (PLM)

Session Code:

Session Code:

ATC22

ATC113A

Room 506

Room 507

This session provides the opportunity for industry leaders and visionaries to report current progress of the continuing advancement in the design,development, and maintenance of aribreathing propulsion systems for current and future aerospace applications. These studies range from examiningunique cycle and fuel concepts to optimizing in-service useage by advanced methods of engine health tracking.

This is session will present papers concerning an adaptive trajectory concept using a fixed-gain set 6-DOF autopilot for a receiver aircraft performingautonomous aerial refueling, an Advanced Flight Control System that will make flying more acceptable for the general public by reducing flight trainingrequirements and provide a strategy automatic avoidance of restricted airspaces and research in improving UAV performance by including the abilityto autonomously detect and exploit thermals in guidance and control algorithms.

Keith Hugus, Belcan Corp.; Laura Mendez, Boeing Co.; H. Robert (Bob) Welge, The Boeing Co.

Reuben M. Chandrasekharan, Bombardier Learjet; Robert A. Stuever, Boeing Integrated DefenseSystems; Jack Terpstra, Cessna Aircraft Co.

Organizers -

Organizers -

1:30 p.m.

2:00 p.m.

2:30 p.m.

3:30 p.m.

4:00 p.m.

4:30 p.m.

2007-01-3932

2007-01-3789

2007-01-3790

2007-01-3816

2007-01-3817

ORAL ONLY

Evaluation of a Mixed Flow Turbofan Engine with Intermediate TurbineBurning for a Supersonic Aircraft

A Mean Value Based Sizing and Simulation Model of a Hydrogen FueledSpark-Ignition Internal Combustion Engine

A Step Towards CO2 Neutral Aviation

Guidance Concept for a Receiver Aircraft to Perform Autonomous AerialRefueling

Implementation of Automatic Airspace Avoidance in an Advanced FlightControl System

Autonomous Soaring

Planned by Propulsion Committee / EMB Air and Space Group


Michael Bergantzel, Mark Waters, California Polytechnic State University

Hongjun Ran, Reid Thomas, Dimitri Mavris, Georgia Institute of Technology

Andreja Brankovic, Robert C. Ryder, Flow Parametrics LLC; Robert C.Hendricks, NASA John Glenn Research Center; Marcia L. Huber, NationalInstitute Standards & Tech.

Kahtan Awni, US Air Force

Kamran Rokhsaz, James Steck, Yakup Gunbatar, Wichita State Univ.

Victor P. Lin, NASA DFRC

Time

Time

Paper No.

Paper No.

Title

Title

3:30 p.m.

1:30 p.m.

Session Time:

Session Time:



Product Lifecycle Management (PLM)Session Code: ATC113B

Room 507

The aerospace industry is growing rapidly and will continue to experience a tremendous growth throughout this decade. To compete and excel intoday's global economy, a distributed virtual enterprises of global teams and partners must be created and function in a highly disciplined, integratedand synchronized fashion. Manufacturers, suppliers and contractors continuously seek new ways to accelerate time to market, improve quality andreliability, ensure compliance, and optimize the use of resources.

The aerospace industry is growing rapidly and will continue to experience a tremendous growth throughout this decade. To compete and excel intoday's global economy, a distributed virtual enterprises of global teams and partners must be created and function in a highly disciplined, integratedand synchronized fashion. Manufacturers, suppliers and contractors continuously seek new ways to accelerate time to market, improve quality andreliability, ensure compliance, and optimize the use of resources.

Joseph J. Barkai, IDC Manufacturing Insights


Organizers -

Organizers -

1:30 p.m.

2:00 p.m.

2:30 p.m.

3:30 p.m.

4:00 p.m.

4:30 p.m.

5:00 p.m.

ORAL ONLY

2007-01-3791

ORAL ONLY

ORAL ONLY

ORAL ONLY

ORAL ONLY

ORAL ONLY

2007-01-3805

Are We There Yet? Review of PLM Maturity and Industry Adoption

Implementing the DoD Unique Identification (UID) Requirement andUnderstanding Its Impact on Manufacturing and Data ManagementSystems

Facilitating Engineering Innovation in a Virtual World

Aircraft Systems and Lifecycle Cost Reduction Potential with DistributedIMA

Prognostics and Health Management: The Joint Strike Fighter's key tosupportability and affordability

Sikorsky's Supplier Collaborative Environment

Enhancing PLM - Bridging the Gap Between Engineering andManufacturing

Advanced Virtualization Technologies in Aerospace and AutomotiveEmbedded System Applications (Written Only -- No Oral Presentation)

Planned by Product Life Management Committee / EMB Air and Space Group

Planned by Product Life Management Committee / EMB Air and Space Group


David E. Roberts, J. Ed McConnell, R. Mark Hudgens, Lockheed MartinAeronautics Co.

Lance Murphy, Dassault Systemes

Mirko Jakovljevic, TTTech. Computertechnik AG

Neal N. McCollom, Lockheed Martin Aeronautics

Richard Parr, Sikorsky Aircraft Corp.

John Cachat, IQS Inc.

Ken Stevens, Travis Siegfried, IBM

Time

Time

Paper No.

Paper No.

Title

Title

3:30 p.m.Session Time:


Noise

Airplane Design for Environment

Session Code:

Session Code:

ATC8

ATC11

Room 510

Room 510

New Manufacturing and material technologies are being utilized in aircraft designs with performance, weight and noise implications. Composites arenow widely used in primary structure requiring new transmission loss treatments. In airplace nacelles, composites are being used to make inletswithout breaks in the acoustic treatment giving improved acoustic performance and weight benefits. Variable geometry technologies are now beingconsidered as enablers for reduced engine source noise. This session will focus on the latest technologies that are reducing current interior, ramp andcommunity noise levels and identify other technologies to enable further reductions.

Session topics include: airframe design space exploration for low noise and low fuel burn, unconventional aircraft concepts with environmentalconsiderations, low emission aircraft design to mitigate climate change and atmospheric impact, and assessment of contrail and cirrus cloud formationon global warming.

David Lee Daggett, Boeing Co.; John William Premo, Boeing Commercial Airplanes

David Lee Daggett, Boeing Co.; Zoltan Spakovszky, Massachusetts Institute of Technology

Organizers -

Organizers -

1:30 p.m.

2:00 p.m.

2:30 p.m.

3:30 p.m.

4:00 p.m.

4:30 p.m.

5:00 p.m.

2007-01-3792

ORAL ONLY

ORAL ONLY

ORAL ONLY

2007-01-3806

2007-01-3807

2007-01-3808

Development of the Acousti-Cap¿ Technology for Double-LayerAcoustic Liners in Aircraft Engine Nacelles

Technology Challenges for Future Aircraft Nacelle Noise andPerformance Improvements

Geared Turbofan Engine Noise Overview

Design Trade Considerations in Noise, Fuel Burn, and TechnologicalRisk for Quiet Aircraft

Development of a Broad Delta Airframe and Propulsion Concepts forReducing Aircraft Noise around Airports

Minimizing Impact on Climate in Aircraft Design

Contrail Avoidance Project Summary

Planned by Environment Committee / EMB Air and Space Group


Asif Ali Syed, Fumitaka Ichihashi, Univ. of Cincinnati; Clark Smith, Earl Ayle,Hexcel Corp.

John William Premo, Boeing Commercial Airplanes

Bruce L. Morin, Pratt & Whitney Aircraft

James I. Hileman, Massachusetts Institute of Technology

Georgios Christos Doulgeris, Cranfield University; Sunil Mistry, CranfieldUniv.; John P. Fielding, Pericles Pilidis, Cranfield University

Regina Egelhofer, Technische Universität München; Christine Bickerstaff,Serge Bonnet, Airbus

Frank Günter Noppel, Riti Singh, Cranfield University

Time

Time

Paper No.

Paper No.

Title

Title

1:30 p.m.

3:30 p.m.

Session Time:

Session Time:




Particulates

Particulates - Panel Discussion

Low Cost Titanium

Session Code:

Session Code:

Session Code:

ATC72A

ATC72B

ATC67

Room 511A - B

Room 511A - B

Room 512

This session will be devoted to presentations and a panel discussion on the current state of the art in our understanding of Particulate Matter (PM)emissions from aircraft. Discussion will focus on current measurement and modeling activities along with challenges that the scientific community isfacing.

This session will be devoted to presentations and a panel discussion on the current state of the art in our understanding of Particulate Matter (PM)emissions from aircraft. Discussion will focus on current measurement and modeling activities along with challenges that the scientific community isfacing.

Because of its combination of high strength, low-density and excellent corrosion resistance, titanium is the material of choice for many applications.The high cost of titanium, however, has prevented significant usage outside of the aerospace, defense, and chemical industries. A number oftechnologies, however, are being developed to reduct the cost of titanium raw material and products.

Anuj Bhargava, Pratt & Whitney; David Lee Daggett, Boeing Co.; Domingo Sepulveda, Pratt &Whitney

Anuj Bhargava, Pratt & Whitney; David Lee Daggett, Boeing Co.; Domingo Sepulveda, Pratt &Whitney

Organizers -

Organizers -

Bruce E. Anderson, NASA; Meredith B. Colket, United Technologies Research Center; Edwin Corporan,Wright-Patterson Air Force Base; Richard C. Miake-Lye, Aerodyne Research Inc.; Philip Whitefield, Univ.of Missouri-Rolla

Panelists -

1:30 p.m.

1:50 p.m.

2:10 p.m.

2:30 p.m.

2:50 p.m.

ORAL ONLY

ORAL ONLY

ORAL ONLY

ORAL ONLY

ORAL ONLY

AFRL Efforts on Aircraft Turbine Engine Emissions

Non-volatile and Volatile Particle Emissions from Aircraft Gas TurbineEngines

Sampling and Characterizing Gas-Turbine Engine Particle Emissions:Problems and Recommended Practices

Evolution of Particle Size Distributions in a Gas Turbine Combustor –Predictions

Aircraft Related PM Research



Edwin Corporan, Wright-Patterson Air Force Base

Richard C. Miake-Lye, Aerodyne Research Inc.

Bruce E. Anderson, NASA

Meredith B. Colket, United Technologies Research Center

Philip Whitefield, Univ. of Missouri-Rolla

Time Paper No. Title

1:30 p.m.

3:30 p.m.

3:30 p.m.

Session Time:

Session Time:

Session Time:



Supply Chain Management


Session Code:

Session Code:

ATC53A

ATC53B

Room 513

Room 513

This Aero-Tech session focuses on supply chain management tools, techniques and opportunities which enhance the flow of materials, parts,products and information throughout the company supply chain. Additionally, this session will address practices that affect supplier performance,quality and foster improved long term relationships among suppliers, partners and customers.


David Amirehteshami, Boeing Phantom Works; Kevin T. Slattery, Boeing Co.

David Amirehteshami, Boeing Phantom Works; Benny J. Leppert, Boeing Co.; Kevin G. Sweeney,Boeing Commercial Airplanes


Organizers -

Organizers -

Organizers -

3:30 p.m.

4:00 p.m.

4:30 p.m.

5:00 p.m.

1:30 p.m.

2:00 p.m.

2:30 p.m.

ORAL ONLY

ORAL ONLY

2007-01-3884

ORAL ONLY

ORAL ONLY

ORAL ONLY

ORAL ONLY

ATI-425 (Ti-4Al-2.5V-1.5Fe-0.25O) a Lower Cost Alternative

Low Cost Titanium Powder Metallurgy Products

An Overview of Titanium Alloys Produced by Electron-Beam Single-Melting (EBSM)

Armstrong Process for Titanium Powder Reduction

Lean Sigma Supply Chain: Secrets of Effective Kanban and LeanScheduling

Supplier Performance

Torino Piemonte Aerospace We Know How

Planned by Manufacturing, Material, Structure Committee / EMB Air and Space Group


John Hebda, Wah Chang

V. S. Moxson, Valad A. Duz, ADMA Products Inc.

Stacey Nyakana, John C. Fanning, Timet Henderson Technical Laboratory

Dariusz Kogut, International Titanium Powder

Jason Premo, nMetric LLC.

John Cachat, IQS Inc.

Diana Giorgini, Centro Estero per I'internazionalizzazione del Piemonte

Time

Time

Time

Paper No.

Paper No.

Paper No.

Title

Title

Title

1:30 p.m.

3:30 p.m.

Session Time:

Session Time:



Thermal Structures

Advanced Composite Fabrication and Joining Processes

Session Code:

Session Code:

ATC68

ATC57

Room 514

Room 514

Concepts and applications, modeling and simulation, test and evaluation, for aerodynamic and thermal load bearing structures for future supersonicair vehicle.

The use of composites for airframe structures continues to increase. With this increase new advances in fabrication and joining are critical to theaerospace industry both military and commerical. This session will concrentrate on advancements in fabrication and joining techniques for compositesstructures in the aerospace industry.

David Amirehteshami, Boeing Phantom Works; Edwin Forster, WPAFB

David Amirehteshami, Boeing Phantom Works; Shaw Lee, Lockheed Martin Aeronautics Co.; RandyA. Southmayd, Boeing Co.

Organizers -

Organizers -

3:30 p.m.

4:00 p.m.

4:30 p.m.

5:00 p.m.

1:30 p.m.

2:00 p.m.

2:30 p.m.

2007-01-3813

ORAL ONLY

ORAL ONLY

ORAL ONLY

2007-01-3794

ORAL ONLY

2007-01-3931

Verification of Supply Chain Quality for Perishable Tools

Hurdling the Obstacles of 3D Design Collaboration

Nadcap - The Highest Level of Quality in Composites: A SmallCompany's Point of View

Mexico Manufacturing Opportunities for the Aerospace Industry

Structural and Thermal Performance Characterization of InsulatedComposite Sandwich Structures

Thermal Analysis of Insulated Fuel Bay in Supersonic Air Vehicle

Through-Thickness Thermal Conductivity in Composites Based on 3-DFiber Architectures



Brian J. Martinek, Boeing Military Airplanes

Jim Merry, Adobe Systems Inc.

Jarrod Ridge, Royal Plastic Mfg Co.

Gale Thompson, The Offshore Group

Edwin Forster, WPAFB

Jonathan D. Bartley-Cho, Northrop Grumman Integrated Systems

Keith W. Sharp, Alexander E. Bogdanovich, 3 Tex Inc.; Jens Schuster, Univ.Of Applied Sciences Kaiserslautern; Dirk Heider, CCM University Of Delware

ORAL ONLY

Time

Time

Paper No.

Paper No.

Title

Title

1:30 p.m.

3:30 p.m.

Session Time:

Session Time:

Wednesday, September 19

Robotics and Component Assy (Part A)Session Code: ATC30

Room 501A - B

Component assembly in the aerospace industry has evolved throughout the years to the extent that succession is pertinent to the advancement oftechnology. A major part of the new technology includes the implementation of some form of robotics.

This Technical Session explores the advanced procedures currently used within industry to enable increased production and quality through roboticapplications. The Robotics and Component Assembly Session will explain various applications related to Lean Manufacturing and advancedtechnologies for today's aircraft assembly processes.

Gordon L. Allen, Steven L. Brisben, Boeing Co.Organizers -

3:30 p.m.

4:00 p.m.

4:30 p.m.

5:00 p.m.

8:00 a.m.

8:30 a.m.

9:00 a.m.

9:30 a.m.

ORAL ONLY

2007-01-3814

ORAL ONLY

ORAL ONLY

2007-01-3815

2007-01-3818

2007-01-3819

2007-01-3820

2007-01-3821

Recent Developments in Polymer Foam Core Materials for Fire ResistantSandwich Constructions and Elevated Temperature Processing

Orbital Drilling of Aerospace Materials

3-D Woven Preform Joint Technology: An Enabler for RobustLightweight Low-Cost Composite Structure

Abrasive Waterjet, The Gold Standard in Composites Machining

Experiencing the Technology Development for High Lifetime Joining ofthe Commercial Aircraft Airframe Components of Metal and PolymerComposite Materials (Written Only -- No Oral Presentation)

High Performance Robotized Assembly System for Challenger 300Business Jet Nose Fuse Panels

Automated Lift Leveling System (ALLS) for 787 Vertical Stabilizer

New PKM Tricept T9000 and Its Application to Flexible Manufacturing atAerospace Industry

Robotic Drilling System for 737 Aileron



Nathan Bruno, DIAB Inc.

Wangyang Ni

Ronald Schmidt, Lee Michael Cooke, Lockheed Martin Aeronautics Co.;Shaw Lee, Lockheed Martin Corp.

Mark Saberton, Flow International Corporation

Georgiy Krivov, Vitaliy Reznikov, Ukrainian Research Institute; Yuri Tarasov,Andrey G. Gromashev, Sukhoi Civil Aviation; Valerij Matvienko, UkrainianResearch Institute

Bruno Monsarrat, National Research Council Canada; Eric Lavoie,Bombardier Aerospace; Gabriel Cote, Martin De Montigny, C. Corbeil,National Research Council Canada; Daniel Grenier, BombardierAeronautique; Xiaowei TU PhD, Dr. Claude Perron, National ResearchCouncil Canada

John P. Barry, Electroimpact Inc.

Jose Luis Olazagoitia, PKMTricept SL; Scott Wyatt, Hartwig Incorporated

Joe Atkinson, John L. Hartmann, Electroimpact Inc.; Simon Jones, PeterGleeson, Boeing-Hawker de Havilland

ORAL ONLY

ORAL ONLY


8:00 a.m.Session Time:




Portable Tooling

Robotics and Component Assy (Part B)

William Littlewood Memorial Lecture

Session Code:

Session Code:

Session Code:

ATC31

ATC32

ATC4

Room 501A - B

Room 501A - B

Room 502A

This sesion will describe innovative application of handheld tools in aircraft manufacturing. Light equipment can be used to preform very accurateprocesses. Their benefits are a significant production cost reduction and improvements in lean manufacturing.

This session focuses on advanced use of robots for automated fastening and assembly. The papers of this session describe both the application ofrobots on current manufacturing processes in aerospace industry as well as proposals for new robotic applications and technology in the near future.

Steven L. Brisben, Gordon L. Allen, Boeing Co.; Sylvain Guerin, Advanced Automation Corp.

Steven L. Brisben, Gordon L. Allen, Boeing Co.; David R. Dotson, Boeing

Edward J. Copeland, NAVAIR; Dennis DeCarlo, Naval Air Warfare Center

Organizers -

Organizers -

Organizers -

2:00 p.m.

2:30 p.m.

3:30 p.m.

4:00 p.m.

4:30 p.m.

5:00 p.m.

2007-01-3849

2007-01-3850

ORAL ONLY

2007-01-3869

2007-01-3870

ORAL ONLY

Advanced Portable Orbital-Drilling Unit for Airbus Final Assembly Lines

Flexible Template for Drill Feed Units

Implementation of Adaptive Control Robot Solutions

Assembly Fixture for 787 Section 11, Heavy Composite Assembly

Snake-Arm Robots: A New Approach to Aircraft Assembly

787 Moving Trailing Edge Assembly System




Benoit Marguet, Frederic Wiegert, Olivier Lebahar, Airbus France; BretrandBretagnol, Assystems; Fahri Okcu, Airbus Germany; Ingvar Eriksson,Eriksson Ingvar, Novator

Axel Wiemann, Scott Leverington, Lubbering GmbH, Lubbering UK

Mark Derren Summers, Airbus UK

Jim Yinger, Dr. Peter B. Zieve, Electroimpact Inc.; Masahiko Nakada, FHILtd.

Rob Buckingham, OCRobotics

Tim Brown, Electroimpact Inc.

Time

Time

Paper No.

Paper No.

Title

Title

1:30 p.m.

3:30 p.m.

10:30 a.m.

Session Time:

Session Time:

Session Time:



Design

Software Design, Tools and Methods

Session Code:

Session Code:

ATC108

ATC1A

Room 503

Room 504

With the advent of open, portable systems technology which has enabled functionally integrated, physically distributed system architectures softwarereuse becomes necessary to remain competitive; but high-level integration and distributed systems have also introduced new challenges for assuringthe system safety. This session examines methods and technology for reusing embedded software, and considers the problem of assuring the safetyof distributed systems in Air Traffic Control applications.

John C. Dalton, Boeing Co.; Steve Wilson, Rockwell Collins Inc.

Mirko Jakovljevic, TTTech. Computertechnik AG; Bob Yeh, Boeing Commercial Airplanes

Organizers -

Organizers -

10:30 a.m.

8:30 a.m.

9:00 p.m.

9:30 p.m.

8:00 a.m.

2007-01-3848

2007-01-3852

2007-01-3871

2007-01-3872

2007-01-3824

2007-01-3873

2007-01-3826

A Business Aircraft View to the Future

System Dependency Analysis for Complex Aircraft Systems

Managing Risk Reduction using a Relative Risk Prioritization Tool

Assuring a Complex Safety-Critical Systems of Systems

Considerations for Using Dual Indication in Aerospace Arc Fault CircuitBreakers (AFCB) (Written Only -- No Oral Presentation)

Rocket Assisted Takeoff (RATO) for Business Jets (Written Only -- NoOral Presentation)

Model-Based Design of Complex Integrated Systems for SynchronuousArchitectures



Preston A. Henne, Gulfstream Aerospace Corp.

Klaus Fritz

Michael Kavoliunas, Bombardier

Steven Beland, Boeing Commercial Airplanes; Ann Miller, Univ. of Missouri-Rolla

Anand Krishnamurthy, Michael J. Lavado, Srini Chandrasekaran, SensataTechnologies

Kent F. Jossie, Cessna Aircraft Co.

Herbert Griebel, TTTech. Computertechnik AG; Bernard Dion, Thierry LeSergent, Bruno Martin, Esterel Technologies

Time

Time

Time

Paper No.

Paper No.

Paper No.

Title

Title

Title

8:00 a.m.

8:00 a.m.

Session Time:

Session Time:



Software Reuse and Safety Assurance

Electro-Optical / Infrared Systems

Session Code:

Session Code:

ATC1B

ATC3

Room 504

Room 504

With the advent of open, portable systems technology which has enabled functionally integrated, physically distributed system architectures softwarereuse becomes necessary to remain competitive; but high-level integration and distributed systems have also introduced new challenges for assuringthe system safety. This session examines methods and technology for reusing embedded software, and considers the problem of assuring the safetyof distributed systems in Air Traffic Control applications.

Mark Lawrence Darnell, GE Aviation; Roscoe C. Ferguson, United Space Alliance; MirkoJakovljevic, TTTech. Computertechnik AG

Mirko Jakovljevic, TTTech. Computertechnik AG

Organizers -

Organizers -

8:30 a.m.

1:30 p.m.

2:00 p.m.

2:30 p.m.

3:30 p.m.

2007-01-3827

ORAL ONLY

2007-01-3854

2007-01-3855

2007-01-3874

Model-Based Development of Distributed Embedded Real-TimeSystems with the DECOS Tool-Chain

Reusable Software Components

Safety Assurance of Distributed System Architecture in Air TrafficControl Applications

Subsystem Design Using Time-Triggered Protocol (TTP): Key Aspectsof Control System Application Reuse

Automatic Control Implementation and Upgraded Electrical SystemDesign for the Oculus 2.0 Sensor Platform



Wolfgang Herzner, Rupert Schlick, Austrian Research Centers GmbH -ARC; Martin Schlager, TTTech Computertechnik AG; Bernhard Leiner,TTTech. Computertechnik AG; Bernhard Huber, Vienna University ofTechnology; Andras Balogh, Gyorgy Csertan, Budapest University ofTechnology and Economics; Alain Le Guennec, Thierry LeSergent, EsterelTechnologies; Neeraj Suri, Shariful Islam, Darmstadt University ofTechnology

Joe Wlad, LynuxWorks

Swapan Mitra, WS Atkins; Giles Pateman, National Air Traffic Services

Roland Wolfig, TTTech. Computertechnik AG

Jay P. Wilhelm

Time

Time

Paper No.

Paper No.

Title

Title

1:30 p.m.

3:30 p.m.

Session Time:

Session Time:



Flying Cars

CFD Applied to Ground Vehicles

Session Code:

Session Code:

ATC20B

ATC16A

Room 505

Room 505

This session will address the development of Personal Transportation vehicles and components, focusing on innovative CTOL and VTOL roadableairplanes and flying automobiles. Required technologies, alternative system configurations, designs under development, prototype hardware, and in-flight performance of remote controlled models and full size prototypes will be presented.

This session is done with the collaboration of the SAE Land & Sea Group. These papers incorporate Computational Fluid Dynamics (CFD) in thedesign of Ground Vehicles. See how CFD is circumventing the traditional wind tunnel process and opt(imiz)ing to go directly to both production andthe road.

Reuben M. Chandrasekharan, Bombardier Learjet; Bruce Harman, Branko Sarh, Boeing Co.

Reuben M. Chandrasekharan, Bombardier Learjet; Paul T. Glessner, Vehicle AerodymanicsConsultants; Gregory K. Watkins, California State University Chico

Organizers -

Organizers -

4:00 p.m.

8:00 a.m.

8:30 a.m.

9:00 a.m.

9:30 a.m.

1:30 p.m.

2:00 p.m.

ORAL ONLY

ORAL ONLY

ORAL ONLY

ORAL ONLY

ORAL ONLY

2007-01-3856

2007-01-3857

EO/IR Technology and Infrared Countermeasure Applications forCommercial Avionics (Invited Paper)

Design Considerations for Autos and Roadable Flying Aircraft

"Door-to-Door" StrongMobile Aircar Project

History and Development of the LaBiche Aerospace FSC-1, Flying Car

How To Win The $300,000 NASA PAV Challenge

Computational Fluid Dynamics Development of the JCB DIESELMAXLand Speed Record Vehicle

CFD Analysis of Directional Stability for the American Challenger RocketCar



Han Le, Univ. of Houston

Palmer C. Stiles

Richard Strong, Safety Analysis Systems Co.

Mitchell LaBiche, Labiche Aerospace

Brien Seeley, CAFE Foundation

Angus Stephen Lock, MIRA, Ltd.

Roshan Oberoi, Sukumar Chakravarthy, Oshin Peroomian, Vedat Akdag,Metacomp Technologies Inc.; William Fredrick, Romatec Engineering; PaulT. Glessner, Vehicle Aerodynamics Consultants, Inc.

Time

Time

Paper No.

Paper No.

Title

Title

8:00 a.m.

1:30 p.m.

Session Time:

Session Time:



CFD Applied to Ground Vehicles

Aerospace Vehicle Systems

Session Code:

Session Code:

ATC16B

ATC62A

Room 505

Room 506

This session is done with the collaboration of the SAE Land & Sea Group. These papers incoroprate Computational Fluid Dynamics (CFD) in thedesign of Ground Vehicles destined to break World Land Speed records. See the both the subsonic and supersonic 'barriers' they will have toovercome.

his session includes technical papers in areas of research, development, test and evaluation of both emergent and fielded technologies related toaerospace vehicle systems. Topics of interest include: systems concept definition, trade studies, technology maturity and insertionopportunities/considerations, theoretical design and analyses, vehicle integration, and life-cycle.

Reuben M. Chandrasekharan, Bombardier Learjet; Paul T. Glessner, Vehicle AerodynamicsConsultants; Gregory K. Watkins, California State University Chico

Rongsheng Li, Boeing Space & Intelligence Systems; Kioumars Najmabadi, Boeing

Organizers -

Organizers -

2:30 p.m.

3:30 p.m.

4:30 p.m.

8:00 a.m.

8:30 a.m.

2007-01-3858

ORAL ONLY

2007-01-3875

2007-01-3829

ORAL ONLY

Racecar Aerodynamic Optimization for an E-1 Class Streamliner UsingArbitrary Shape Defromation

Optimization of Aerodynamic Design for Supermileage Vehicle

Methodology for Optimizing the Aerodynamic Performance of the TimeAttack Series Cobb Tuning Subaru WRX 2006 Using Mesh DeformationTechniques

A Novel Tool for the Conceptual Design of Aircraft On-Board PowerSystems

Microbial Influenced Corrosion (MIC) The Causes, Effects, Cures &Detection Methods for the Aviation Industry



Miles Jackson, Optimal Solutions Software, LLC; Barrett Taylor Newill, PerryCarter, Brigham Young University

Himanshu Almadi, Maruti Udyog, Ltd.; Sagar Maji, Delhi College ofEngineering

Matthew Cross, Advantage CFD; Miles Jackson, Optimal Solutions, LLC

Christian Schallert, DLR

Howard L. Chesneau, Edward English, Fuel Quality Services Inc.

Time

Time

Paper No.

Paper No.

Title

Title

3:30 p.m.

8:00 a.m.

Session Time:

Session Time:



Novel Propulsion Technologies

Novel Propulsion Technologies

Session Code:

Session Code:

ATC37A

ATC37B

Room 506

Room 506

This session explores new-to-the-world or unexploited propulsion technologies that fall within the scope of the SAE Propulsion Committee, i.e., airbreathing engines and space launch systems. This encompasses innovative propulsion system and engine concepts (including related aspects of airvehicle integration), and original approaches to thrust generation and augmentation, propulsion cycle functions (compression, combustion & powerextraction) and subsystems. Subsystems topics may include unusual fuels and fuel treatments, breakthrough control systems and electrical powergeneration, and new departures in lubrication and mechanical systems. Novel methods for test and evaluation, including instrumentation, will beconsidered.

Richard C. Millar, NAVAIR; H. Robert (Bob) Welge, The Boeing Co.Organizers -

9:00 a.m.

1:30 p.m.

2:00 p.m.

2:30 p.m.

2007-01-3828

2007-01-3830

2007-01-3859

2007-01-3860

2007-01-3861

Concept Development of a Pneumatically Driven, Fixed Root CirculationControlled Helicopter

Doing More with Less: Weight-Optimized Electric Actuation Systems(Written Only -- No Oral Presentation)

Status, Vision, and Challenges of an Intelligent Distributed EngineControl Architecture

Soviet Propeller V/STOL Concepts of the 20th Century

Application of Non-Parametric Statistical Methods to ReliabilityDatabase Analysis

Planned by Aerospace Vehicle Systems Committee / EMB Air and Space Group


Gerald M. Angle, Center for Ind. Research, West Virginia Univ.; Emily D.Pertl, Franz A. Pertl, James E. Smith, Center for Ind. Research Applications,West Virginia Univ.

Ingolf Schaefer, Harmonic Drive AG

Alireza R. Behbahani, Air Force Research Lab.; Dennis Culley, NASA JohnGlenn Research Center; Bert J. Smith, Christopher Darouse, US Army;Richard C. Millar, NAVAIR; Bruce Wood, Jim Krodel, Pratt & Whitney;Sheldon Carpenter, William Mailander, GE Aircraft Engines; Timothy DavidMahoney, Ron Quinn, Honeywell; Colin Patrick Bluish, Bobbie Hegwood,Rolls-Royce Corp.; Gary Battestin, Walter Roney, BAE Systems; WilliamRhoden, Hamilton Sundstrand; William Storey, Goodrich

Michael J. Hirschberg, CENTRA Technology, Inc.; Thomas Mueller, AviationHistorian

Richard C. Millar, US Navy-NAVAIR; Thomas Mazzuchi, Shahram Sarkani,George Washington University


1:30 p.m.

3:30 p.m.

Session Time:

Session Time:



Maintenance/Operations


Session Code: ATC109A

Room 507

This session explores new-to-the-world or unexploited propulsion technologies that fall within the scope of the SAE Propulsion Committee, i.e., airbreathing engines and space launch systems. This encompasses innovative propulsion system and engine concepts (including related aspects of airvehicle integration), and original approaches to thrust generation and augmentation, propulsion cycle functions (compression, combustion & powerextraction) and subsystems. Subsystems topics may include unusual fuels and fuel treatments, breakthrough control systems and electrical powergeneration, and new departures in lubrication and mechanical systems. Novel methods for test and evaluation, including instrumentation, will beconsidered.

This session will explore processes, tools and methods for improving aviation maintenance and operations safety. Increasing the effectivity andefficiency of maintenance processes and the use of engineering controls redesign are reviewed. Diagnostic tools for fiber optics, aviation batteries,fluid leaks and engine gearbox and generators are explored and analytical methods on usage of mean-time-between-failure (MTBF) values,electrostatic discharge effects on airborne avionics and language based risk factors are presented.

Richard C. Millar, NAVAIR; H. Robert (Bob) Welge, the Boeing Co.

John C. Dalton, Boeing Co.; Eric M. Peterson, Honeywell International Inc.

Organizers -

Organizers -

3:30 p.m.

4:00 p.m.

4:30 p.m.

5:00 p.m.

8:00 a.m.

8:30 a.m.

9:00 a.m.

ORAL ONLY

2007-01-3876

ORAL ONLY

ORAL ONLY

2007-01-3831

2007-01-3832

2007-01-3833

U-Turn Aerospace Plane

Liquid Oxygen/Liquid Methane Rocket Engine Development

Mass Injected Pre-Compressor Cooling (MIPCC) of Gas Turbine Engines

JENTEC, RM 8 Advanced Performance Rocket Engine

Usage of MTBF for Exposure Times of Undetected Faults in SafetyAssessments

Wireless Devices Usage with Adaptive Interfaces in the Context ofAeronautical Maintenance Processes to Reduce the Incidence of theHuman Error and Increase Safety

Electrostatic Discharge Phenomenon: A Potential Threat to AircraftSafety




Charl E. Janeke

Daniel L. Delong, Jeffrey K. Greason, Khali Rodway Mckee, XCORAerospace

Robert J. Engers, Alliant Techsystems

Dale Jenson, JENTEC

Eric M. Peterson, Honeywell International Inc.; Hals N. Larsen, FederalAviation Administration

Francesco Gargiulo, Italian Aerospace Research Center

Fidele Moupfouma, Bombardier Inc.

Time

Time

Paper No.

Paper No.

Title

Title




Session Code:

Session Code:

ATC109B

ATC109C

Room 507

Room 507





Organizers -

Organizers -

1:30 p.m.

2:30 p.m.

3:30 p.m.

4:00 p.m.

4:30 p.m.

5:00 p.m.

ORAL ONLY

2007-01-3863

2007-01-3862

2007-01-3877

2007-01-3878

2007-01-3879

ORAL ONLY

2007-01-3880

Leak Detection in Explosive and Non-explosive Environments using aTracer Gas

Optical Backscatter Reflectometry as a Measurement Tool for Fiber-Optics in Avionics and Aerospace Applications

Co-Evolution of Military Vehicles and Their Fire Extinguishing Systems(Written Only -- No Oral Presentation)

Ground and On-Board Diagnostics and Prognostics for AircraftBatteries

Very High Frequency Monitoring System for Engine Gearbox andGenerator Health Management

Evaluation of Aircraft Slide Evacuation Injuries

Safety Management System (SMS) and its Implications for theManufacturing Sector

Miscommunication in Aviation Contexts: A Perspective from SpeechMove Schemes (Written Only -- No Oral Presentation)


Richard Mizia, Alcatel

Stephen t. Kreger, Brian J. Soller, Dawn Gifford, Roger G. Duncan, MatthewS. Wolfe, Mark E. Froggatt, Luna Technologies

Steven E. Hodges, Kidde Aerospace & Defense

John E. James, B.Y. Tsenter, Gem Power LLC

Matthew J. Watson, Carl Byington, Impact Technologies LLC; Alireza R.Behbahani, Air Force Research Lab.

Vahid Motevalli, Layla Monajemi, Maryline Rassi, George Washington Univ.

Tom Garcia, Culture Dynamcis

Wen-ling Tsai, Shih Chien University

ORAL ONLY

CANCELLED

Time

Time

Paper No.

Paper No.

Title

Title

1:30 p.m.

3:30 p.m.

Session Time:

Session Time:



Aerospace Operations I

Aerospace Operations II

Session Code:

Session Code:

ATC111A

ATC111B

Room 510

Room 510

Aerospace is rapidly evolving with advanced knowledge and information technologies. This session will present modeling, simulation, and autonomyconcepts and technologies to provide increased performance, reliability, survivability and safety in aerospace operations and systems.

Aerospace is rapidly evolving with advanced knowledge and informaiton technologies. This session will present modeling, simulation, and autonomyconcepts and technologies to provide increased performance, reliability, survivability and safety in aerospace operations and systems.

Jorge Bardina, NASA Ames Research Center; Luis Rabelo, Univ. of Central Florida


Organizers -

Organizers -

8:00 a.m.

8:30 a.m.

9:00 a.m.

9:30 a.m.

1:30 p.m.

2:00 p.m.

2:30 p.m.

2007-01-3834

2007-01-3835

ORAL ONLY

2007-01-3836

2007-01-3864

ORAL ONLY

2007-01-3865

Workforce Enterprise Modeling

Collaborative Network Centric Experiment Involving Joint Services andNorthrop Grumman Corporation

Data Mining for Aeronautics Integrated Vehicle Health Management

Integrated Use of Data Mining and Statistical Analysis Methods toAnalyze Air Traffic Delays

Case for a Multidisciplinary Modeling Platform for Space Launch RiskAnalysis

Key Technologies on the Virtual Test Bed for Launch and RangeOperations

Decision Support Systems for Launch and Range Operations Using Jess


Planned by Man-Machine Interface Committee / EMB Air and Space Group


Mario F. Marin, Yanshen Zhu, American Technologika LLC; Phillip Meade,Melissa Sargent, Julie Warren, NASA

Robert P. Smerke, Northrop Grumman; Howard Lacey, Northrop GrummanCorp.

Nikunj Chandrakant Oza, NASA Ames Research Center

Deepak Kulkarni, NASA Ames Research Center

Serge N. Sala-Diakanda, Luis C. Rabelo, Jose A. Sepulveda, Univ. ofCentral Florida

Jorge Bardina, NASA Ames Research Center

Rajkumar Thirumalainambi, PSGS @ NASA Ames Research Center

Time

Time

Paper No.

Paper No.

Title

Title

8:00 a.m.

1:30 p.m.

Session Time:

Session Time:



Aerospace Operations III

Materials & Processes

Session Code:

Session Code:

ATC111C

ATC10

Room 510

Room 511A - B


Regulations, customer requirements, and individual corporate goals are driving the aerospace industry to validate alternatives to materials of concern.Many application for cadmium and hexavalent chromium have high preformance and reliability requirements that create a significant challenge forpotential substitutions. This session will highlight some of the alternatives being tested.


David Lee Daggett, Boeing Co.; Erin K. Yaeger, Pratt & Whitney

Organizers -

Organizers -

3:30 p.m.

4:00 p.m.

4:30 p.m.

5:00 p.m.

8:00 a.m.

8:30 a.m.

9:00 a.m.

ORAL ONLY

2007-01-3881

2007-01-3882

2007-01-3883

2007-01-3837

ORAL ONLY

ORAL ONLY

Intelligent Flight Systems: Progress and Potential of this Technology

First Results: FORAS in Operation

Idealized Modeling and Analysis of Shuttle Wing Leading Edge ImpactData

Sealing and Structural Enhancement System for the Rear Cargo Ramp ofa C-130 Aircraft

Zn-Ni Plating as a Cadmium Alternative

Diffused Nickel-Cadmium Electroplate Replaced By Diffused Nickel-Zinc

Development and Implementation of a Chromate-Free Pre-Paint SurfaceTreatment for Boeing Commercial Airplanes


James M. Urnes, Boeing Aircraft Co.

Michael Hadjimichael, US Naval Research Laboratory

Upender K. Kaul, NASA Ames Research Center

Zenovy S. Wowczuk, West Virginia University (CIRA); Kenneth ArthurWilliams, West Virginia Univsity (CIRA); James E. Smith, West VirginiaUniversity (CIRA)

Tetsuo Taniguchi, Hidefumi Saito, Shimadzu Corp.; Masamichi Yamada,Sumitomo Precision Products Co., Ltd.; Hajime Iobe, Fuji Heavy Industries,Ltd.; Koji Takada, Takada Laboratories Inc.; Michimasa Yoshida, DipsolChemcials; Eri Sato, Asahi Kinzoku Kogyo Co., Ltd.; Taichi Ishihara, MEIRACorp.

Thomas R. Hanlon, Pratt & Whitney

Kay Y. Blohowiak, Randall Jahren, Mark J. Johnson, Joseph Osborne, JillSeebergh, Boeing Co.

Time

Time

Paper No.

Paper No.

Title

Title

3:30 p.m.

8:00 a.m.

Session Time:

Session Time:



Energy

Energy

Session Code:

Session Code:

ATC7A

ATC7B

Room 511A - B

Room 511A - B

Enabling alternate fuels for aviation. The emphasis is on commerical aviation fuels that can supplement or replace current crude oil derived kerosenejet fuels.

Enabling alternate fuels for aviation. The emphasis is on commerical aviation fuels that can supplement or replace current crude oil derived kerosenejet fuels.

Edwin Corporan, Wright-Patterson Air Force Base; David Lee Daggett, Boeing Co.

Edwin Corporan, Wright-Patterson Air Force Base; David Lee Daggett, Boeing Co.

Organizers -

Organizers -

9:30 a.m.

1:30 p.m.

2:00 p.m.

2:30 p.m.

3:30 p.m.

4:00 p.m.

4:30 p.m.

ORAL ONLY

ORAL ONLY

2007-01-3866

2007-01-3867

ORAL ONLY

ORAL ONLY

ORAL ONLY

Replacements for Aerospace Materials of Concern: Technical Maturityand Knowledge Gaps

Air Force Alternative Fuels Program

The Commercial Aviation Alternate Fuels Initiative

U.S. DOE Fossil Energy Fuel Cell Program

Alternative Fuels & Emissions - A Perspective from the AviationIndustry

Progress of Alternate Fuels for Commercial Aircraft

A Breakthrough Approach to Produce Commercially Viable AviationBiofuel




Mark Jaworowski, United Technologies Research Center

Edwin Corporan, Wright-Patterson Air Force Base

David Lee Daggett, Oren Hadaller, The Boeing Commercial Airplane Group;Lourdes Maurice, Mark Rumizen, Nathan Brown, Federal AviationAdministration; Richard Altman, CAAFI Executive Director; HowardAylesworth, Aerospace Industries Association

Wayne Surdoval, U.S. DOE National Energy Technolgy Lab.

Myrka Manzo, Air Canada

David Lee Daggett, Boeing Co.

Jeff H. Hassannia, Diversified Energy Corp.

Time

Time

Paper No.

Paper No.

Title

Title

1:30 p.m.

3:30 p.m.

Session Time:

Session Time:



Advanced Metal Materials, Fabrication and Joining Processes

Robotized Processes Simulation

Session Code:

Session Code:

ATC51B

ATC44

Room 512

Room 512

Advancements in the production of metallic structure continues to be important to the aerospace and commerical aviation industries. This sessionfeatures improved materials, processes and joining methods for metallic components to meet the challenges put forth by demanding end productrequirements.

The session will highlight state-of-the-art practices in the aerospace industry using digital manufacturing software. Topics will range from productspecification to process design and resources off-line programming with applications in fields such as automated fastening and robotizedmanufacturing.

David Amirehteshami, Boeing Phantom Works; Jeffrey D. Morgan, Boeing Commercial Airplanes

David Amirehteshami, Boeing Commercial Airplanes; Bruno Monsarrat, National Research CouncilCanada

Organizers -

Organizers -

8:00 a.m.

8:30 a.m.

9:30 a.m.

1:30 p.m.

2:00 p.m.

2:30 p.m.

2007-01-3812

2007-01-3838

2007-01-3839

2007-01-3868

ORAL ONLY

ORAL ONLY

Performance Evaluation of 2-mm Thick Alclad AA2024 T3 AluminiumAlloy Friction Spot Welding

Reducing Corrosion Fatigue and SCC Failures in 300M Steel LandingGear Using Low Plasticity Burnishing

Advanced Low-cost Titanium-alloy Materials for Aerospace FastenerApplications

Parallel Kinematic Assisted Automated Assembly

Digital Manufacturing for the Automated Flexible Development Cell

Model-Based Robot Path Generation for Surface Treatment Applications



Antonio A.M. Da Silva, Institute for Matls. Research,GKSSForschungszentrum GmbH; Jorge Dos Santos, Institute for Matls. Research,GKSS Forschungszentrum GmbH; Tonilson Rosendo, Institute for Matls.Research,GKSS Forschungszentrum GmbH; F. D. Ramos, C.C. P.Mazzaferro, Institute for Matls. Research, GKSS Forschungszentrum GmbH;M.A. D. Tier, L. Bergmann, Universidada Regional Integrada do AltoUruguai Das Missoes; J.A. E. Mazzaferro, DEMEC UFRGS; T.R.Strohaecker, PPGEM UFRGS

Doug J. Hornbach, Paul S. Prevey, Lambda Technologies Inc.

Steven G. Keener, Boeing Co.

Colm Joseph Higgins, Queens Univ.; Mark Derren Summers, HarveyBrookes, Airbus UK

Luke J. Huckin, Airbus UK; Roger Holden, Metris UK, Ltd.

Jason Michel Lambert, Simon Larose, Claude Perron, National ResearchCouncil Canada; Pierre Drouin, Ecole Polytechnique Montreal

ORAL ONLY

Time

Time

Paper No.

Paper No.

Title

Title

8:00 a.m.

1:30 p.m.

Session Time:

Session Time:



Advanced Metal Materials, Fabrication and Joining Processes


Session Code:

Session Code:

ATC51A

ATC53C

Room 512

Room 513

Advancements in the production of metallic structure continues to be important to the aerospace and commerical aviation industries. This sessionfeatures improved materials, processes and joining methods for metallic components to meet the challenges put forth by demanding end productrequirements.


David Amirehteshami, Boeing Phantom Works; Jeffrey D. Morgan, Boeing Commercial Airplanes


Organizers -

Organizers -

3:30 p.m.

4:00 p.m.

4:30 p.m.

8:00 a.m.

8:30 a.m.

9:00 a.m.

9:30 a.m.

2007-01-3809

2007-01-3810

2007-01-3811

ORAL ONLY

ORAL ONLY

2007-01-3840

2007-01-3841

Re-Engineering, Austempering, and Selective Laser Hardening of a 4340Latch Body used in the Cargo Hook of a CH-47 Military Helicopter

Literature Data and Corrosion Testing of Hard Anodized and DuplexSealed 7075-T7351 and 7050-T7451 Wrought Aluminum Alloy Platesafter Cyclic Loading

Robotic Friction Stir Welding

AS9100: What's the Point?

AS 9100 Quality Systems

Monitoring Environmental Conditions by Leveraging Advanced RadioFrequency Identification (RFID)

What Goes into Your Parts is More Important than Where You SourceThem



Winston Sequeira, Mike Jensen, Eric Peterson, Steven Thieman, AlionMcNally Center for Production Technologies

Winston Sequeira, Mike Jensen, Eric Peterson, Steven Thieman, AlionMcNally Center for Production Technologies

Georg Voellner, iwb, TU Muenchen; J. Silvanus, EADS Innovation WorksGermany; Otto Kellenberger Ing, Kuka Roboter GmbH

Grant Obrien, SGS

Dan Urbaniak, Worldwide Quality Network

George Nicholas Bullen, Northrop Grumman Corproation; Tim Shinbara,Northrop Grumman

Trevor Stansbury, Supply Dynamics

Time

Time

Paper No.

Paper No.

Title

Title

3:30 p.m.

8:00 a.m.

Session Time:

Session Time:




Lean Manufacturing

Lean Manufacturing

High Output Composite Manufacturing

Session Code:

Session Code:

ATC52A

ATC52B

Room 513

Room 513

This Aero Tech session targets applications of lean manufacturing principals, practices and methodologies throughout the value stream. Although thesession is focused primarily on lean tools principally in manufacturing, it might also include the application of lean principal, practices andmethodologies that add value and eliminate waste in the design or office enviornment as well.

This Aero Tech session targets applications of lean manufacturing principals, practices and methodologies throughout the value stream. Although thesession is focused primarily on lean tools principally in manufacturing, it might also include the application of lean principal, practices andmethodologies that add value and eliminate waste in the design or office enviornment as well.



Organizers -

Organizers -

1:30 p.m.

2:00 p.m.

2:30 p.m.

3:30 p.m.

4:00 p.m.

4:30 p.m.

ORAL ONLY

ORAL ONLY

ORAL ONLY

2007-01-3885

2007-01-3886

ORAL ONLY

Managing Value Stream Risk

Lean Sigma Blitz: Continuous Improvement in 1/2 the time throughCollaborative Manufacturing

Product Quality Validation: A System for Production and DeliverySchedule Risk Reduction

Process Simulation Ensures the Flexibility of AIRBUS' New Moving Line

Kaizen Through Heijunka Production (Leveled Production)

Driving "Total Accounted Cost" - Lean Design



Michael J. Dreikorn, IPL Group LLC

Jason Premo, Cernotec

Donald Jasurda, QMC LLC

Lutz Spiekermann, AIRBUS CIMPA GmbH; Jan Westphal, AirbusDeutschland

Katsuya Koide, Takeshi Iwata, Shingijutsu Global Consulting USA Inc.

David Foreman, Design Profit Inc.

Time

Time

Paper No.

Paper No.

Title

Title

1:30 p.m.

3:30 p.m.

Session Time:

Session Time:



Integrated Structural Health Monitoring

Multifunction and Adaptive Structures

Session Code:

Session Code:

Session Code:

ATC55

ATC70

ATC69

Room 514

Room 514

Room 514

As composite materials move into primary structure on large aircraft, composite structures are getting much larger in physical size. Automatedprocesses with high lbs-per-hour lay up rates are required to build these large structures. This session will focus on automated processes used tobuild larger aircraft composite structural componets.

This session includes contributions to the health monitoring of structural systems. Topics include, but not limited to the following areas- healthmonitoring in machinery; structural health diagnostics; applications to aerospace vehicles, automotive vehicles, ship and submarines, among others;nondestructive inspections and examination (NDI and NDE) techniques; sensor and sensor networks; algorithms for damage detection andmonitoring.

This session will explore the possibilities of the adaptive and multifunctional structures of the furture.

David Amirehteshami, Boeing Phantom Works; Carroll G. Grant, Aerospace Composites Consulting

David Amirehteshami, Boeing Phantom Works; Ramesh Kolar, Naval Postgraduate School

David Amirehteshami, Boeing Phantom Works; Richard Coveno, US Air Force; Jerry Huang, BoeingPhantom Works

Organizers -

Organizers -

Organizers -

8:00 a.m.

8:30 a.m.

9:00 a.m.

2:00 p.m.

2:30 p.m.

2007-01-3842

2007-01-3843

ORAL ONLY

ORAL ONLY

ORAL ONLY

Medium Wave Infrared Heater for High-Speed Fiber Placement

High-Speed Fiber Placement on Large Complex Structures

Recent Advancements in Fiber Placement Technology

US Navy Roadmap to Structural Health and Usage Monitoring ThePresent and Future

Structural Health Monitoring for High-Speed Naval Ships



Rick Calawa, John Nancarrow, Electroimpact Inc.

Russell Devlieg, Kyle A. Jeffries, Peter Vogeli, Electroimpact Inc.

Luis Izco, Javier Isturiz, M Torres Group; Manu Motilva, Mtorres Group

Scott Maley, US Navy

Liming W. Salvino, Naval Surface Warfare Center; Paul Hess, ONR (Officeof Naval Research)

Time

Time

Time

Paper No.

Paper No.

Paper No.

Title

Title

Title

8:00 a.m.

1:30 p.m.

3:30 p.m.

Session Time:

Session Time:

Session Time:



Guidance & Control

OEM Systems Updates

Session Code:

Session Code:

ATC42

ATC39

Room 518

Room 518

This session considers a sensor fusion approach using traditional IMU/GPS sensors with vision to facilitate the state estimation problem of movingtargets; coordinating a diverse group of UAVs to observe the battlespace, update digital maps, and annotate recorded activity; a newly developedtheory for the dynamics and control of maneuvering flexible, light weight UAVs, which are expected to carry out maneuvers well in excess of whatpilots are able to tolerate and a new generation of flight control systems based on boundary layer control with micro-strakes and canards, activeporosity devices, and solid-state plasma actuators.

Piergiovanni Marzocca, Clarkson Univ.; Jack Terpstra, Cessna Aircraft Co.

Piergiovanni Marzocca, Clarkson Univ.; Scott A. Nelson, SAE International

Organizers -

Organizers -

3:30 p.m.

4:00 p.m.

4:30 p.m.

8:00 a.m.

8:30 a.m.

9:00 a.m.

9:30 a.m.

ORAL ONLY

ORAL ONLY

ORAL ONLY

2007-01-3844

2007-01-3845

2007-01-3846

2007-01-3847

Quantum Leap in Design & Development Tools

Magnetoelectrics a New Approach for Structural Antennas

Structural Health Monitoring for Aerospace Applications

Dynamic Target State Estimation for Autonomous Aerial Vehicles usinga Monocular Camera System

Coordinated Autonomous UAVs: Applications for a HeterogeneousUrban RSTA Team

Mission Planning for UAV Sensing Tasks in Close ProximityEnvironments

Aerionics - A New Aero Industry for Flight Control


Planned by Flight Sciences Committee / EMB Air and Space Group; Unmanned Aerial Vehicle Committee / EMB Air and SpaceGroup

Dr. James P. Hubner, University Of Alabama; Todd Gross, Wissam El-Ratal, Lambert Technologies LLC

Greg P. Carman, Univ. of California

Jerry Huang, Boeing Phantom Works

Ryan Scott Causey, Siddhartha S. Mehta, Rick Lind, Warren Dixon,University of Florida

Caroline King, William Koenig, Air Force Research Lab.

Joseph Kehoe, Rick Lind, University of Florida

Robert N. Schmidt, Orbital Research Inc.; Mehul P. Patel, AerodynamicsGroup, Orbital Research Inc.

Time

Time

Paper No.

Paper No.

Title

Title

8:00 a.m.

1:30 p.m.

Session Time:

Session Time:


Thursday, September 20

Civil & Military Aircraft

Advanced Fastening Systems and Hole Generation

Session Code:

Session Code:

ATC13

ATC33

Room 518

Room 501A - B

This session offers a variety of paper topics, from an overview of the Boeing 747-Large Cargo Freighter development program, to potential designsolutions for challenging missions, operations, and unconventional aero-propulsion general arrangements.

Fasteners and the tools used to install them have been evolving for hundreds of years. Advancements in materials, coatings, and hole generationhave enabled fastening technologies to support the high performance requirements of today's aerospace industry. The quest for ever lighter, higherperformance, environmentally friendly fastening systems continues to drive innovation and development. This session will cover examples of newfastening materials, coatings, processes, and quality hole generation.

Reuben M. Chandrasekharan, Bombardier Learjet; Chester P. Nelson, Boeing CommercialAirplanes

Steven L. Brisben, Gordon L. Allen, Boeing Co.; Daniel Thurnau, Spirit AeroSystems Inc.

Organizers -

Organizers -

1:30 p.m.

2:00 p.m.

3:30 p.m.

4:00 p.m.

8:00 a.m.

8:30 a.m.

9:00 a.m.

ORAL ONLY

ORAL ONLY

2007-01-3888

2007-01-3889

2007-01-3890

2007-01-3893

2007-01-3892

Persistent High Altitude ISR - Global Hawk System Update

Shadow Systems Update

The 747-400 Dream Lifter - Overview & Mission

Columned Multi Bubble Fuselage (CMBF) for BWB

Influence of Fastener Coatings on Fretting Fatigue

Drilling Advanced Aircraft Structures with PCD (Poly-CrystallineDiamond) Drills

Test Results of Electrodeposited Cadmium Alternatives for ThreadedFastener Applications

Planned by Unmanned Aerial Vehicle Committee / EMB Air and Space Group; Flight Sciences Committee / EMB Air and SpaceGroup


Alfredo Ramirez, Northrop Grumman Corp.

S. Kristi Moe, AAI Corp.

Christopher C. Funke, Boeing Commercial Airplanes

Sung Hwan Cho, The Sir Lawrence Wackett Centre for Aerospace Design;Cees Bil, RMIT University

Cindie Giummarra, Harry Zonker, Alcoa Technical Center; Liang Zeng, LukeHaylock, Alcoa Fastening Systems

Richard Garrick, Precorp

Mark W. Smith, Lockheed Martin Aeronautics Co.CANCELLED

Time

Time

Paper No.

Paper No.

Title

Title

3:30 p.m.

8:00 a.m.

Session Time:

Session Time:



Advancements In Auto Fastening

Secure Aeronautical Communications / Safety and Security Certification

Session Code:

Session Code:

ATC34

ATC110C

Room 501A - B

Room 503

This session is dedicated to the advancements in automation in the fields of drilling, riveting, bolting, and welding.

A safety design process approach will be presented. This approach may also be used as an augmentation to existing standards such as DO-178B/254 software development process.

Steven L. Brisben, Gordon L. Allen, Boeing Co.; Paul Thompson, Electroimpact Inc.

John C. Dalton, Boeing Co.; Donald C. Kauffman, Honeywell International Inc.; Andy Wallington, GEAviation (formerly Smiths Aerospace)

Organizers -

Organizers -

9:30 a.m.

10:30 a.m.

11:00 a.m.

11:30 a.m.

12:00 p.m.

2007-01-3891

2007-01-3913

2007-01-3914

2007-01-3915

2007-01-3916

2007-01-3917

Optimization of Split Sleeve Cold Expansion Process for AerospaceAluminum Alloys

One Piece Barrel Fastening

Process Development for 787 Doors Assemble

Automated Riveting Cell for A320 Wing Panels with ImprovedThroughput and Reliability (SA2)

Development of an Automated Part Loading and Unloading System for aCylindrical Die Thread Roller

Implementation of Low-Cost Technologies in Sustaining Production(Written Only -- No Oral Presentation)





Frederic Barlat, Alcoa; Cindie Giummarra, M. E. Karabin, Robert Schultz,Alcoa Technical Center

Naoya Hiratsuka, Tsuyoshi Osawa, Kawasaki Heavy Industries, Ltd.;Michael Assadi, Rick Calawa, Scott Smith, Scott Tomchick, ElectroimpactInc.; Makoto Nitta, Fuji Industries, Ltd.

Philippe Prat, Alema Automation

Ray Holden, Electroimpact Inc.; Paul Haworth, Electroimpact Ltd.; IanKendrick, Andrew Smith, Airbus UK Ltd.

Matthew Wagner, Shreyes Melkote, John Morehouse, Georgia Institute ofTechnology; Forrest Curtis Lea, Guzmaro Romero, Phat Lam, AlcoaFastening Systems; Steve L. Dickerson, Camotion Inc.

James A. Johnson, David A. Gonzalez, Lockheed Martin Aeronautics

ORAL ONLY


10:30 a.m.

8:00 a.m.

Session Time:

Session Time:



Guidance Navigation & Flight Controls

Navier-Stokes CFD Codes

Session Code:

Session Code:

ATC107

ATC17

Room 504

Room 505

This session includes paper on aircraft guidance, navigation and flight control algorithms and hardward.

Navier-Stokes CFD codes have been in intensive development for a number of years, as tools for the numerical simulation of viscous, compressibleflows. In recent years, a number of CFD codes have found widespread application, particularly in the aerospace & process industries, thanks to thedevelopment of low cost computing platforms. This session will cover examples of the industrial application of Navier-Stokes codes, as well as themethodologies behind some of these codes.

Gary Balas, Univ. of Minnesota; Mirko Jakovljevic, TTTech. Computertechnik AG; Demetri Tsamis,Rockwell Collins Inc.

Reuben M. Chandrasekharan, Bombardier Learjet; Chittur S. Venkatasubban, Raytheon Aircraft Co.

Organizers -

Organizers -

8:00 a.m.

8:30 a.m.

9:00 a.m.

8:30 a.m.

9:00 a.m.

9:30 a.m.

10:00 a.m.

2007-01-3897

2007-01-3918

2007-01-3919

2007-01-3898

2007-01-3899

2007-01-3900

2007-01-3901

Safety and Security Certification: An Approach to Accomplish

Digital Identities: Finally Becoming A Reality

Industry Activities Related to Aircraft Information Security

Hybrid Adaptive Flight Control with Self-Improving Plant Model forStability and Control of Damaged Aircraft

Adaptive Control of Unmanned Aerial Vehicles in Atmospheric Flightwith Reduced Models

An Electro-Mechanical Actuator for General Aviation Aircraft

Investigation of Signal Jitter in COTS Optical Tracking Devices for usewith Synthetic Vision Systems



Francois W. Guay, Ensco Inc.

John Pawlicki, SITA

Roy T. Oishi, ARINC Inc.; Michael Olive, Honeywell; Steve Arentz, UnitedAirlines Inc.

Nhan Nguyen, NASA Ames Research Center

Nazli E. Kahveci, Petros A. Ioannou, University of Southern California; MajD. Mirmirani, California State University, Los Angeles

S. Hesse, G. Konrad, Reinhard Reichel, Univ. of Stuttgart; Ingolf Schaefer,P. Bourlier, M. Buff, Harmonic Drive AG

Schinnel Small, Morgan State University; Kofi Nyarko, Morgan State Univ.

CANCELLED

ORAL ONLY

Time

Time

Paper No.

Paper No.

Title

Title

8:00 a.m.

8:00 a.m.

Session Time:

Session Time:



Certification and Vehicle Control Issues


Session Code:

Session Code:

ATC25

ATC62B

Room 505

Room 506

This session was designed for certification and controllability issues for manned and unmanned aerial vehicles. Certification covers regulations,standards and verifications addressing safety of the aircraft, crew, and passengers throughout its operational flight envelop. Controllability issuescover the flight control system from cockpit input to surface output including governing subsystems in software and hardware.

This session includes technical papers in areas of research, development, test and evaluation of both emergent and fielded technologies related toaerospace vehicle systems. Topics of interest include: systems concept definition, trade studies, technology maturity and insertionopportunities/considerations, theoretical design and analyses, vehicle integration, and life-cycle.

Kahtan Awni, US Air Force; Reuben M. Chandrasekharan, Bombardier Learjet; Jack Terpstra,Cessna Aircraft Co.


Organizers -

Organizers -

8:00 a.m.

8:30 a.m.

9:00 a.m.

9:30 a.m.

10:30 a.m.

11:00 a.m.

11:30 a.m.

ORAL ONLY

ORAL ONLY

ORAL ONLY

ORAL ONLY

2007-01-3920

2007-01-3921

2007-01-3922

Navier-Stokes and CFD Studies for the CRJ-900 LR Winglets Design

Navier-Stokes CFD Technology Applied to the Hawker-850XP BusinessJet.

An Overview of Flow Simulation Capabilities of CFD

Aerodynamic Analysis and Design using the NSU3D Unstructured

Active Flow and Aeroelastic Control of Lifting Surfaces Using SyntheticJet Actuators

Robust Analysis of Active Flutter Suppression Using Multiple ControlSurfaces via Second-Order Controllers

Safety and Certification of UAVs



Fassi Kafyeke, Bombardier Aerospace

Chittur S. Venkatasubban, Hawker Beechcraft Corporation

Sukumar Chakravarthy, Metacomp Technologies Inc.

Dimitri J. Mavriplis, Univ. of Wyoming

Piergiovanni Marzocca, M. Stolk, K. O'Donnell, Clarkson Univ.; Roeland DeBreuker, Tudelft; M. Abdalla, E. Nicolini, Z. Gurdal, Delft Univ. of Technology

Ying Teng, Boeing Co.

Rebecca Menes, Herbert Hecht, SoHaR Inc.

Time

Time

Time

Paper No.

Paper No.

Paper No.

Title

Title

Title

10:30 a.m.

8:00 a.m.

Session Time:

Session Time:




Aerospace Operations: Wireless Integrated Cockpit Information Display

Session Code:

Session Code:

ATC62C

ATC112

Room 506

Room 510

This session includes technical papers in areas of research, development, test and evaluation of both emergent and fielded technologies related toaerospace vehicle systems. Topics of interest include: systems concept definition, trade studies, technology maturity and insertionopportunities/considerations, theoretical design and analyses, vehicle integration, and life-cycle.



Jorge Bardina, NASA Ames Research Center; Jose Sepulveda, Univ. of Central Florida; RajkumarThirumalainambi, PSGS @ NASA Ames Research Center

Organizers -

Organizers -

8:00 a.m.

8:30 a.m.

9:00 a.m.

10:30 a.m.

8:00 a.m.

8:30 a.m.

9:00 a.m.

2007-01-3902

2007-01-3903

ORAL ONLY

ORAL ONLY

2007-01-3904

2007-01-3905

ORAL ONLY

Impact of Oscillatory Failure Cases in Electro-Hydraulic ActuationSystems on an Aeroelastic Aircraft

Power and Thermal Management Integration

Lunar Rocket and Rover / JENTEC SpaceStation Supply Vehicle

Applying Robust Methods to Achieve Maximum Reliability of AerospacePower Systems Designs

Wireless Integrated Cockpit Information Display: The UnderlyingTechnologies

Wireless Integrated Cockpit Information Display: Military CockpitApplications

Wireless Integrated Cockpit Information Display: Demonstration



Helge Sachs, Hamburg University of Technology; Udo B. Carl, FrankThielecke, Institute of Aircraft Systems Engineering

Yuhang Ho, Northrop Grumman Corp.

Dale Jenson, Robert Kleinberger, JENTEC

John P. Huber, Michael Jensen, Synopsys Inc.

Ryan Eggert, Chris Sielski, Derryl A. Williams, US Air Force

Chris Sielski, Ryan Eggert, Derryl A. Williams, US Air Force ResearchLaboratory

Ryan Eggert, Christopher Sielski, US Air Force Research Laboratory

ORAL ONLY

Time

Time

Paper No.

Paper No.

Title

Title

10:30 a.m.

8:00 a.m.

Session Time:

Session Time:



Environmental Control Systems

Emissions

Session Code:

Session Code:

ATC9

ATC6A

Room 510

Room 511A - B

Enviromental Control Systems (ECS) for heating, cooling and cabin pressurization in commerical aircraft.

A total of six papers will be presented including three on recent advances in propulsion engine emissions reduction in addition to the three dealingwith:A hybrid fuel cell/battery propulsion system comprised of lithium-ion batteries with a proton exchange membrane fuel cell as the main power sourceand supplies sufficient electrical power for level flight has been developed and demonstratedUse of renewable sources of energy including biomass, wind, solar thermal, and photovoltaic to emissions offset equivalency for ground energyproduction and use to offset air space emissions.Modeling paper on NOx, CO2, and Physical Particulate Reduction in a Swirled-Air, Liquid-Fuel Combustion Chamber.

David Lee Daggett, Boeing Co.; Paul H. McMurtry, Hamilton Sundstrand

David Lee Daggett, Boeing Co.; Hukam Mongia, GE Aviation; Domingo Sepulveda, Pratt & Whitney

Organizers -

Organizers -

10:30 a.m.

11:00 a.m.

11:30 a.m.

12:00 p.m.

8:00 a.m.

ORAL ONLY

2007-01-3923

ORAL ONLY

2006-01-2562

ORAL ONLY

Flow Balancing and Optimization Techniques for Environmental ControlSystems

Advanced Environmental Control System (The 2nd Part)

Boeing 787 Dreamliner - Creating a Superior Cabin Environment forPassengers and Crew

Aircraft Cabin Thermal Comfort Evaluation Using Numerical Manikins

Air Vehicle Emissions Offset With Onground Renewable EnergyResources



Ron Esmao, Flowmaster USA Inc.

Hidefumi Saito, Shimadzu Corp.; Yukio Kamiyoshihara, Takafumi Kawadu,Japan Aircraft Development Corp.; Kay Takao, Mitsubishi Heavy Industries,Ltd.; Tadashi Ueda, Masahiro Ohshima, Kawasaki Heavy Industries, Ltd.;Toru Iwata, Tokyo Aircraft Instrument Co., Ltd.

Matthew Schwab, Boeing Commercial Airplanes

Fernando Stancato, Embraer-Empresa Brasileira Aero SA; Arlindo Tribess,Tales Andriano Ferreira, Dario Abilio Cruz, Gustavo Simoes Arujo, EscolaPolitecnica Univ. Sao Paulo; Luis C. Santos, Embraer-Empresa BrasileiraAero SA

Jaswant Toor PE, San Diego

*

Time

Time

Paper No.

Paper No.

Title

Title

10:30 a.m.

8:00 a.m.

Session Time:

Session Time:



Metal Additive Manufacturing

Advanced Robotics Applications

Session Code:

Session Code:

ATC50

ATC48

Room 512

Room 512

This session is directed toward exploring progress toward fabrication metal parts directly from the CAD file using any of a number of additivemanufacturing methods. This category of manufacturing is being explored to reduct cost and weight as well as to directly produce parts which couldnot be manufactured by conventional means without using inordinately long manufacturing cycles and consuming very long lead times.

David Amirehteshami, Boeing Phantom Works; Ralph E. Anderson, Pratt & Whitney

David Amirehteshami, Boeing Phantom Works; Roger Holden; Claude Perron, National ResearchCouncil Canada

Organizers -

Organizers -

8:30 a.m.

9:00 a.m.

9:30 a.m.

8:00 a.m.

8:30 a.m.

9:00 a.m.

10:30 a.m.

2007-01-3906

ORAL ONLY

ORAL ONLY

ORAL ONLY

ORAL ONLY

ORAL ONLY

ORAL ONLY

The Boeing Fuel Cell Demonstrator Airplane

NOx, CO2, and Physical Particulate Reduction in a Swirled-Air, Liquid-Fuel Combustion Chamber Using CFD with Combustion Capabilities anda Physical Model

TALON X Low NOx Combustor Overview

Status Report on Ni Superalloy Electron Beam Deposition withMicrostructural Control

Progress in Maturation and Qualification of Deposited Ti6Al4V

Process Modeling and Prediction for Laser Metal Deposition

Evolution of Shot Peening Induced Surface Roughness and ResidualStresses



Nieves Lapeña-Rey, Jonay Mosquera, Elena Bataller, Fortunato Orti,Boeing Research & Technology Europe, Environmental Tech.

Christian A. Dominguez, MFDC Laboratory

James B. Hoke, UTC-Pratt&Whitney

Ralph E. Anderson, Keystone Synergistic Enterprises, Inc.

V. Blake Slaughter, Boeing

Zhiqiang Fan, Frank Liou, University of Missouri-Rolla; Kevin Slattery,Boeing Phantom Works; Mary Kinsella, AFRL/MLLMP; Joseph Newkirk,University of Missouri-Rolla; Hsin-Nan Chou, Boeing Phantom Works

Simon Larose, National Research Council Canada; Hong Yan Miao, EcolePolytechnique Montreal; Claude Perron, National Research Council Canada

Time

Time

Paper No.

Paper No.

Title

Title

8:00 a.m.

10:30 a.m.

Session Time:

Session Time:



Design/ Utilization of Process Capability Information

Analysis and Modeling Tools

Session Code:

Session Code:

ATC58

ATC59

Room 513

Room 513

The presentations in this session will describe how to effectively collect and utilize process capability data. The authors will discuss what data shouldbe collected, how it is analyzed and stored to used effectively to reduce costs and imporve product quality.

Airfram design and certification requires thorough investigation of physical system behavior, identification of all failure modes, and quantification of allsafety margins. To meet modern performance criteria, these certification requirements require advanced analysis and modeling tools that efficientlyand effectively leverage the knowledge of structural analysts. The presentations in this track highlight such tools and discuss their application toaerospace programs and research.

David Amirehteshami, Boeing Phantom Works; James A. Day, Boeing Co.

David Amirehteshami, Boeing Phantom Works; Ramesh Kolar, Naval Postgraduate School; RobertoF. Lu, Boeing Commercial Airplanes; Robert Taylor, Lockheed Martin Aeronautics Co.

Organizers -

Organizers -

11:00 a.m.

11:30 a.m.

8:00 a.m.

8:30 a.m.

9:00 a.m.

ORAL ONLY

ORAL ONLY

2007-01-3907

2007-01-3908

ORAL ONLY

3D Random Finite Element Model for Shot Peening Process

Determination of Shot Peening Coverage based on a Visual InspectionSystem

Identify/Utilize Process Capability Information to Predict Variation inAircraft Early Design

A New Simulation Technique Using a Holistic Approach andMethodology to Assess Productivity of a New Plant for Manufacturingthe Boeing 787

Dimensional Process Capability Information (PCI) for increasedprofitability.



H. Y. Miao, Ecole Polytechnique Montreal; Simon Larose, National ResearchCouncil Canada; M. Levesque, Ecole Polytechnique Montreal; ClaudePerron, National Research Council Canada

Xiaowei TU, Simon Larose, Claude Perron, National Research CouncilCanada

Zuozhi Zhao, Michelle Bezdecny, Byungwoo Lee, Dean Robinson, GeneralElectric R D; Lowell Bauer; Mark Slagle, Richard Coleman, John Barnes,Stephen Walls, Boeing Co.

Marco Pissarello, Riccardo DiBattista, Technoplants SpA; Paolo Falletti,Alenia Aeronautica SpA

Anna Thornton, Analytics Operations Engineering; Stephen Walls, BoeingCo.

Time

Time

Paper No.

Paper No.

Title

Title

8:00 a.m.

10:30 a.m.

Session Time:

Session Time:



Metrology and Automation Systems

Design

Session Code:

Session Code:

ATC114

ATC40A

Room 514

Room 518

Metrology and automation control system developments have made great strides in recent years. This session will present and discuss the applicationand potential applications of these systems in aerospace manufacture. It will present current metrology uses for control of assemblies, potentialmetrology systems and also discuss automation control system developments to lower capital requirements in machining systems.

David Amirehteshami, Boeing Phantom Works; Phillip J. Crothers, Hawker de HavillandOrganizers -

10:30 a.m.

11:00 a.m.

11:30 a.m.

12:00 p.m.

12:30 p.m.

8:00 a.m.

8:30 a.m.

9:00 a.m.

ORAL ONLY

ORAL ONLY

2007-01-3925

2007-01-3926

ORAL ONLY

2007-01-3927

2007-01-3909

ORAL ONLY

ORAL ONLY

A Finite Element Analysis Based Analytical Model for Rapid Screeningof Snap-Through Buckling in Aircraft Structures

Rapid Spreadsheet Methodology to Generate Loads-Based StructuralWeights for Aircraft Conceptual Design

A Software Method for Demonstrating Validation of Computer DummyModels Used in the Evaluation of Aircraft Seating Systems

Developments in Hole-to-Hole Assembly

Structural Analysis and Optimization on the F-35 Lightning II

Reducing Design Time, Part Cost, and Manufacturing Risk on NewAirplane Projects Using Intelligent Software Solutions (Written Only --No Oral Presentation)

On the Use of Force Feedback for Cost Efficient Robotic Drilling

A.C.P. Integration Discussion on Precision Gantry Machine Tools withVolumetric and Thermal Compensation

Geometry Assurance in Airframe Manufacturing and Assembly



Alex S. Selvarathinam, Lockheed Martin Fort Worth Co.

Robert Olliffe, Lockheed Martin Aeronautics Co.

Dirk Twisk, Peter Ritmeijer, TNO Automotive Safety Solutions

Jeroen Bloem, Stork Fokker AESP BV

Robert Taylor, Lockheed Martin Aeronautics Co.

Peter A. Schoot, Boeing Co.; Keith M. Badgley, Dan Christiansen, MeishelleHaverkamp, Vykor

Henrik Kihlman, Linkoping University; Torgny Brogardh, ABB Robotics;Mathian Haage, Klas Nilsson, Tomas Olsson, Lund University

Mark Wingrove, ACP Machinery

Richard Lindqvist, Saab Aerostructures


8:00 a.m.

8:00 a.m.

Session Time:

Session Time:


DesignSession Code: ATC40B

Room 518

This session deal with a new type of design for a small rugged and low-cost UAV accounting for new construction techniques and new materials; thedevelopment of a balloon launched UAS with telescopic wing with improved performance and aerial vehicle remote sensing capabilities foratmospheric and other near space research; the design, development, testing and integration of inflatable UAVs wings with unconventional controlsurfaces allowing for a large design space and possible mission adaptability; the development of image exploitation system and image processingalgorithms and techniques to process real time video and flight data acquired by a UAV for military and civilian applications for surveillance, searchand rescue missions

This session deal with the evaluation of range and flight maneuvering performance of a UAV considered during its conceptual design phase; thedesign and development of a long endurance hybrid PEM fuel cell powered small UAV with an aerodynamically efficient composite airframeconstructed of carbon and fiberglass; the design, testing and qualification of a parachute recovery system for UAVs; the mission planning task andalgorithms development for small UAV sensing missions in urban operations with the scope of providing potential solution strategies to maximizesensor effectiveness.

Kahtan Awni, US Air Force; Piergiovanni Marzocca, Clarkson Univ.; Jack Terpstra, Cessna AircraftCo.

Kahtan Awni, US Air Force; Piergiovanni Marzocca, Clarkson Univ.; Jack Terpstra, Cessna AircraftCo.

Organizers -

Organizers -

8:00 a.m.

8:30 a.m.

9:00 a.m.

9:30 a.m.

10:00 a.m.

10:30 a.m.

ORAL ONLY

2007-01-3910

2007-01-3911

ORAL ONLY

ORAL ONLY

2007-01-3912

2007-01-3930

A Low Cost, Rapid Construction Unmanned Aircraft Design

Balloon Launched UAV with Nested Wing for Near Space Applications

Expanding the Small UAV Design Space with Inflatable Wings

Structural Design Criteria for Military UAV

Hypersonic Freighter

Image Exploitation System for Airborne Surveillance (Written Only -- NoOral Presentation)

Development of a Small Long Endurance Hybrid PEM Fuel Cell PoweredUAV


Thomas A. Bateman, Northrop Grumman Integrated Systems

David E. Gevers, Gevers Aircraft Inc.; Margaret M. Ratcliff, James A. Hatch,Purdue University

Jamey D. Jacob, Oklahoma State Univ.; Suzanne Smith, Univ. of Kentucky;David Cadogan, Steven Scarborough, ILC Dover LP

Wolfgang Luber, EADS Airbus GmbH

Dale Jensen, Robert Kleinberger, JENTEC

P. Karunakaran, Frederick Mathews, S. H. Padmanabhan, HCLTechnologies, Ltd.

Christopher Herwerth, California State University, Los Angeles; CharlesChiang, Alan Ko, Shigeru Matsuyama, Sang Bum Chio, California StateUniv-Los Angeles; Maj Mirmirani, California State University-Los Angeles;Dustin Gamble, Ryan Paul, Valentin Sanchez, Andrew S. Arena, OklahomaState University; Author Koschany, George Gu, Taras Wankewycz, PlacidoJin, Horizon Fuel Cell Technologies

Time

Time

Paper No.

Paper No.

Title

Title


11:00 a.m.

11:30 a.m.

12:00 p.m.

12:30 p.m.

2007-01-3928

2007-01-3929

ORAL ONLY

ORAL ONLY

The Selection and Qualification of a Parachute Recovery System forYour UAV

Robust Control Design for a Flexible Unmanned Aerial Vehicle

Development of a Process for Certification of Military UAV Systems inthe US National Airspace System (NAS)

Wireless Energy Delivery to Structural Health Monitoring Sensor Nodesby Unmanned Aerial Vehicles


Manley C. Butler, Roberto Montanez, Butler Parachute Systems Inc.

Ilhan Tuzcu, Univ. of Alabama

Gene Kelly, Certtech LLC; Leslie Alford, Boeing Co.

Austin P. Mascarenas; Michael Todd, Univ. of California-San Diego

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